Hornung, Hans

Book Chapter from CaltechAUTHORS

Finch, Peter M. and Schwartz, Tal, et el. (2023) Near-Body Measurements in Hypersonic Wedge Flows in the T5 Reflected Shock Tunnel by Tunable Diode Laser Absorption Spectroscopy; ISBN 978-1-62410-699-6; AIAA SCITECH 2023 Forum; Art. No. 2023-2518; 10.2514/6.2023-2518
Yu, Wesley M. and Austin, Joanna M., et el. (2022) Freestream Static Pressure Measurements in the T5 Reflected Shock Tunnel; 10.2514/6.2022-1658
Finch, Peter M. and Schwartz, Tal, et el. (2022) Near-Body Measurements in Hypersonic Cylinder Flows in the T5 Reflected Shock Tunnel by Tunable Diode Laser Absorption Spectroscopy; ISBN 978-1-62410-631-6; AIAA Scitech 2022 Forum; Art. No. 2022-1705; 10.2514/6.2022-1705
Girard, Julian and Finch, Peter M., et el. (2021) Characterization of the T5 Reflected Shock Tunnel Freestream Temperature, Velocity, and Composition using Laser Absorption Spectroscopy; ISBN 978-1-62410-611-8; AIAA Propulsion and Energy 2021 Forum; Art. No. 2021-3525; 10.2514/6.2021-3525
Schwartz, Tal and Girard, Julian, et el. (2021) Characterization of the Caltech Hypervelocity Expansion Tube via Tunable Diode Laser Absorption Spectroscopy; ISBN 978-1-62410-611-8; AIAA Propulsion and Energy 2021 Forum; Art. No. 2021-3524; 10.2514/6.2021-3524
Finch, Peter M. and Girard, Julian, et el. (2020) Measurements of Time-Resolved Air Freestream Nitric Oxide Rotational, Vibrational Temperature and Concentration in the T5 Reflected Shock Tunnel; ISBN 978-1-62410-602-6; AIAA Propulsion and Energy 2020 Forum; Art. No. 2020-3714; 10.2514/6.2020-3714
Hannemann, Klaus and Itoh, Katsuhiro, et el. (2015) Free Piston Shock Tunnels HEG, HIEST, T4 and T5; ISBN 978-3-319-23744-2; Experimental Methods of Shock Wave Research; 181-264; 10.1007/978-3-319-23745-9_7
Parziale, N. J. and Schmidt, B. E., et el. (2015) Pulsed Laser Diode for Use as a Light Source for Short-Exposure, High-Frame-Rate Flow Visualization; ISBN 9781624103438; AIAA SciTech : 53rd AIAA Aerospace Sciences Meeting; Art. No. 2015-0530; 10.2514/6.2015-0530
Parziale, N. J. and Shepherd, J. E., et el. (2015) Geometric Acoustics in High-Speed Boundary Layers; ISBN 978-3-319-16834-0; 29th International Symposium on Shock Waves; 711-716; 10.1007/978-3-319-16835-7_114
Hornung, Hans G. (2014) Mach Reflection in Steady Flow. I. Mikhail Ivanov's Contributions, II. Caltech Stability Experiments; ISBN 978-0-7354-1265-1; Proceedings of the 29th International Symposium on Rarefied Gas Dynamics; 1384-1393; 10.1063/1.4902753
Schmidt, B. E. and Bitter, N. P., et el. (2014) Experimental Investigation of Gas Injection into the Boundary Layer on a Slender Body in Supersonic Flow; ISBN 978-1-62410-293-6; 7th AIAA Theoretical Fluid Mechanics Conference; Art. No. 2014-2496; 10.2514/6.2014-2496
Parziale, N. J. and Shepherd, J. E., et el. (2013) Differential Interferometric Measurement of Instability at Two Points in a Hypervelocity Boundary Layer; ISBN 9781624101816; 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition; Art. No. 2013-0521; 10.2514/6.2013-521
Parziale, N. J. and Rabinovitch, J., et el. (2012) A Proposed Vertical Expansion Tunnel; ISBN 9781600869334; 42nd AIAA Fluid Dynamics Conference and Exhibit; Art. No. 2012-3263; 10.2514/6.2012-3263
Parziale, N. J. and Shepherd, J. E., et el. (2012) Reflected Shock Tunnel Noise Measurement by Focused Differential Interferometry; ISBN 9781600869334; 42nd AIAA Fluid Dynamics Conference and Exhibit; Art. No. 2012-3261; 10.2514/6.2012-3261
Marineau, Eric and Hornung, Hans (2012) Heat Flux Calibration of T5 Hypervelocity Shock Tunnel Conical Nozzle in Air; ISBN 978-1-60086-973-0; 47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition; Art. No. 2009-1158; 10.2514/6.2009-1158
Karl, Sebastian and Hannemann, Klaus, et el. (2012) Bluntness Effects in Hypersonic Flow over Slender Cones and Wedges; ISBN 978-3-642-25684-4; 28th International Symposium on Shock Waves; 691-696; 10.1007/978-3-642-25685-1_105
Hornung, Hans G. and Schramm, Jan Martinez, et el. (2012) Sonic Line and Stand-Off Distance on Re-entry Capsule Shapes; ISBN 978-3-642-25684-4; 28th International Symposium on Shock Waves; 605-611; 10.1007/978-3-642-25685-1_92
Parziale, N. J. and Jewell, J. S., et el. (2012) Shock Tunnel Noise Measurement with Resonantly Enhanced Focused Schlieren Deflectometry; ISBN 978-3-642-25687-5; 28th International Symposium on Shock Waves; 747-752; 10.1007/978-3-642-25688-2_113
Marineau, Eric C. and Laurence, Stuart J., et el. (2010) Apollo-Shaped Capsule Boundary Layer Transition at High-Enthalpy in T5; ISBN 9781600869594; 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition; Art. No. 2010-446; 10.2514/6.2010-446
Marineau, Eric C. and Hornung, Hans G. (2010) Study of Bow-Shock Wave Unsteadiness in Hypervelocity Flow from Reservoir Fluctuations; ISBN 9781600869594; 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition; Art. No. 2010-382; 10.2514/6.2010-382
Wagnild, Ross M. and Candler, Graham V., et el. (2010) Carbon Dioxide Injection for Hypervelocity Boundary Layer Stability; ISBN 978-1-60086-959-4; 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition; Art. No. 2010-1244; 10.2514/6.2010-1244
Leyva, Ivett A. and Jewell, Joseph S., et el. (2009) On the impact of injection schemes on transition in hypersonic boundary layers; ISBN 9781600869686; 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference; Art. No. 2009-7204; 10.2514/6.2009-7204
Marineau, Eric C. and Hornung, Hans G. (2009) High-Enthalpy Nonequilibrium Nozzle Flow of Air: Experiments and Computations; ISBN 9781600869716; 39th AIAA Fluid Dynamics Conference; Art. No. 2009-4216; 10.2514/6.2009-4216
Sanderson, Simon R. and Austin, Joanna M., et el. (2009) Reactant Jetting in Unstable Detonation; ISBN 1-56347-975-3; 39th AIAA Fluid Mechanics Conference; Art. No. -2009-4325; 10.2514/6.2009-4325
Hornung, H. G. (2009) Relaxation effects in hypervelocity flow: selected contributions from the T5 Lab; ISBN 9783540851677; Shock Waves; 3-10; 10.1007/978-3-540-85168-4_1
Marineau, Eric C. and Hornung, Hans G. (2009) Modeling and Calibration of Fast-Response Coaxial Heat Flux Gages; ISBN 978-1-60086-973-0; 47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition; Art. No. 2009-737; 10.2514/6.2009-737
Leyva, Ivett A. and Laurence, Stuart, et el. (2009) Transition Delay in Hypervelocity Boundary Layers by Means of CO₂/Acoustic Instability Interactions; ISBN 978-1-60086-973-0; 47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition; Art. No. 2009-1287; 10.2514/6.2009-1287
Mouton, C. A. and Hornung, H. G. (2009) Experimental investigation of tripping between regular and Mach reflection in the dual-solution domain; ISBN 9783540851806; Shock Waves; 1413-1418; 10.1007/978-3-540-85181-3_100
Laurence, S. J. and Deiterding, R., et el. (2009) Tandem spheres in hypersonic flow; ISBN 9783540851677; Shock Waves; 713-718; 10.1007/978-3-540-85168-4_115
Hornung, H. G. (2008) Deriving Features of Reacting Hypersonic Flows from Gradients at Curved Shocks; ISBN 978-1-60086-995-2; 5th AIAA Theoretical Fluid Mechanics Conference; Art. No. 2008-4340; 10.2514/6.2008-4340
Hornung, H. G. and Mouton, C. A. (2008) Some More on Transition Between Regular and Mach Reflection of Shock Waves in Steady Flow (Invited); ISBN 978-1-60086-989-1; 38th Fluid Dynamics Conference and Exhibit; Art. No. 2008-3845; 10.2514/6.2008-3845
Hornung, Hans G. (2006) Hypersonic Real-Gas Effects on Transition; ISBN 978-1-4020-4149-5; IUTAM Symposium on One Hundred Years of Boundary Layer Research; 335-344; 10.1007/978-1-4020-4150-1_32
Shepherd, J. E. and Hornung, H. G. (2005) Blast Waves and Explosions Sound generation by explosive decompression of an airplane; ISBN 978-3-540-22497-6; Shock Waves; 973-978; 10.1007/978-3-540-27009-6_148
Leyva, I. A. and Hornung, H. G. (2000) Shock Detachment Process in Hypervelocity Flow over a Cone; ISBN 085432707X; Proceedings of the 22nd International Symposium on Shock Waves; 1607-1612; 10.7907/GRNB-AA64
Bélanger, J. and Hornung, H. (1995) Transverse Jet Mixing and Combustion Experiments in the Hypersonic Shock Tunnel T5 at GALCIT; ISBN 978-3-642-78831-4; Shock Waves @ Marseille I - Hypersonics, Shock Tube & Shock Tunnel Flow; 157-162; 10.1007/978-3-642-78829-1_25
Germain, P. and Hornung, H. (1995) The Boundary Layer on a Sharp Cone in High-Enthalpy Flow; ISBN 978-3-642-78831-4; Shock Waves @ Marseille I - Hypersonics, Shock Tube & Shock Tunnel Flow; 63-68; 10.1007/978-3-642-78829-1_9
Wen, Chihyung and Hornung, Hans (1995) Experiments on Hypervelocity Dissociating Flow over Spheres; ISBN 978-3-642-78834-5; Shock Waves @ Marseille II - Physico-Chemical Processes and Nonequilibrium Flow; 223-228; 10.1007/978-3-642-78832-1_37
Hornung, H. G. and Germain, P. (1995) An Exploratory Study of Transition on a Slender Cone in Hypervelocity Flow; ISBN 9783642797675; Laminar-Turbulent Transition; 155-162; 10.1007/978-3-642-79765-1_18
Hornung, H. and Wen, C., et el. (1994) Hypervelocity flow over spheres; ISBN 978-3-211-82495-5; Fluid- and Gasdynamics; 163-170; 10.1007/978-3-7091-9310-5_19
Hornung, H. and Sturtevant, B., et el. (1992) Performance data of the new free-piston shock tunnel T5 at GALCIT; ISBN 978-3-642-77650-2; Shock Waves; 603-610; 10.1007/978-3-642-77648-9_95
Hornung, H. G. (1989) Concluding Remarks; ISBN 9783642835865; Symposium Transsonicum III; 501-504; 10.1007/978-3-642-83584-1_40
Hornung, Hans (1985) The effect of viscosity on the mach stem length in unsteady strong shock reflection; ISBN 978-3-540-15989-6; Flow of Real Fluids; 82-91; 10.1007/3-540-15989-4_73
Hornung, Hans and Killen, Peter (1977) Laboratory study of a stationary oblique plunging breaker for surfboard testing; ISBN 978-3-540-08253-8; Waves on Water of Variable Depth; 121-128; 10.1007/3540082530_143